High Speed Aerodynamics detailed syllabus for Aeronautical Engineering (Aero) for 2021 regulation curriculum has been taken from the Anna Universities official website and presented for the Aero students. For course code, course name, number of credits for a course and other scheme related information, do visit full semester subjects post given below.
For Aeronautical Engineering 5th Sem scheme and its subjects, do visit Aero 5th Sem 2021 regulation scheme. For Professional Elective-II scheme and its subjects refer to Aero Professional Elective-II syllabus scheme. The detailed syllabus of high speed aerodynamics is as follows.
Course Objectives:
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Unit I
FUNDAMENTAL ASPECTS OF COMPRESSIBLE FLOW
Compressibility, Continuity, Momentum and energy equation for steady one dimensional flow-compressible Bernoulli’s equation-Calorically perfect gas, Mach Number, Speed of sound, Area – Mach number – Velocity relation, Mach cone, Mach angle, One dimensional Isentropic flow through variable area duct, Static and Stagnation properties, Critical conditions, Characteristic Mach number, Area-Mach number relation, Maximum discharge velocity.
Unit II
SHOCK AND EXPANSION WAVES
Normal shock relations, Prandtl’s relation-Hugoniot equation, Raleigh Supersonic Pitot tube equation-Moving normal shock waves, Oblique shocks, 0-p-M relation, Shock Polar, Reflection of oblique shocks, left running and right running waves-Interaction of oblique shock waves, slip line, Rayleigh flow, Fanno flow, Expansion waves, Prandtl-Meyer expansion, Maximum turning angle, Simple and non-simple regions, operating characteristics of Nozzles, under expansion, over expansion.
Unit III
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Unit IV
HIGH SPEED FLOW VvER AIRFOILS, WINGS AND AIRPLANE
CONFIGURATION
Critical Mach number, Drag divergence Mach number, Shock Stall, Supercritical Airfoil Sections, Transonic area rule, Swept wing, Airfoils for supersonic flows, Lift, drag, Pitching moment and Centre of pressure for supersonic profiles, Shock expansion theory, wave drag, supersonic wings, Design considerations for supersonic aircrafts.
Unit V
CHARACTERIZATION OF HIGH SPEED FLOWS
Shock-Boundary layer interaction, Wind tunnels for transonic, Supersonic and hypersonic flows, shock tube, Gun tunnels, Supersonic flow visualization, Introduction to Hypersonic Flows.
Course Outcomes:
- Analyze the effect of compressibility at high-speeds and to make intelligent design decisions based on this understanding.
- Analyse about shock waves and expansion waves.
- Calculate 2D compressible flows.
- Estimate the high speed flow over airfoils and wings.
Text Books:
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Reference Books:
- Oosthuizen,P.H., &Carscallen,W.E., Compressible Fluid Flow, CRC Press; 2nd edition (July 22, 2013)
- Shapiro, A. H., Dynamics and Thermodynamics of Compressible Fluid Flow, Ronald Press, 1982.
- Zucrow, M. J. and Anderson, J. D., Elements of Gas Dynamics, McGraw- Hill &Co., 1989.
For detailed syllabus of all the other subjects of Aeronautical Engineering 5th Sem, visit Aero 5th Sem subject syllabuses for 2021 regulation.
For all Aeronautical Engineering results, visit Anna University Aero all semester results direct link.